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Current Issue

  • 2010,Vol 31,No. 5

    15 May 2010

Simulation and optimization design of hybrid rocket motor

2010, 31 (5): 513-518   

Distribution of surge waves at inlet exit section for a aeroengine

2010, 31 (5): 519-522   

Investigation on mechanism of low frequency combustion instabilities in a dump combustor

2010, 31 (5): 523-528   

The stability of solid rocket motor chamber under lateral pressure

2010, 31 (5): 529-532   

A study on the flowfield of a z-flowpath combustor

2010, 31 (5): 533-538   

Effects of backpressure on spray cone of liquid swirl injector

2010, 31 (5): 539-543   

Influence of combustion stabilization by primary rocket under commix-combustion mode in RBCC

2010, 31 (5): 544-548   

Experiments of integrated aeroramp injector/gas-portfire in a supersonic combustion

2010, 31 (5): 549-554   

Investigation of the flow mechanisms of affecting compressor performance with axial skewed slots casing treatment

2010, 31 (5): 555-561   

Unsteady behavior of tip clearance flow in an axial flow compressor rotor at near stall condition

2010, 31 (5): 562-566   

Numerical simulation of the trailing edge cooled transonic turbine aerodynamic characteristic

2010, 31 (5): 567-571   

Afterburning Fuel Flow Optimal Control

2010, 31 (5): 572-575   

Experiments on HTPB propellant aging properties under constant strain

2010, 31 (5): 576-580   

Stress relaxation modulus calculation based on dynamic master curve of storage modulus for solid propellants

2010, 31 (5): 581-586   

Molecular dynamics simulation of interaction between GAP grafted hydantoin and solid oxidizers in for GAP propellant

2010, 31 (5): 587-592   

Computation for the flow and heat transfer properties of a pin fin duct

2010, 31 (5): 593-598   

Experimental study of deflective theory of film cooling trajectory under rotating operating conditions

2010, 31 (5): 599-605   

Numerical investigation of turbulent heat transfer of cryogenic-propellant methane under supercritical pressures

2010, 31 (5): 606-611   

Experiment on ablation characteristic of EPDM insulator under particles erosion condition

2010, 31 (5): 612-617   

Experiment on ablation of EPDM insulator simulating overload condition

2010, 31 (5): 618-622   

Simulation of propellant ablation and conduction of pulsed plasma thruster

2010, 31 (5): 623-628   

Performance investigation on pulse detonation engine using dynamic mesh method

2010, 31 (5): 629-633   

Two-dimensional numerical simulation of rotating detonation wave engine

2010, 31 (5): 634-640